CN209097013U - Unmanned plane and inclining rotary mechanism - Google Patents
Unmanned plane and inclining rotary mechanism Download PDFInfo
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- CN209097013U CN209097013U CN201821572617.0U CN201821572617U CN209097013U CN 209097013 U CN209097013 U CN 209097013U CN 201821572617 U CN201821572617 U CN 201821572617U CN 209097013 U CN209097013 U CN 209097013U
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- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64C—AEROPLANES; HELICOPTERS
- B64C27/00—Rotorcraft; Rotors peculiar thereto
- B64C27/52—Tilting of rotor bodily relative to fuselage
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Abstract
The utility model discloses a kind of unmanned plane and inclining rotary mechanisms, are related to aviation aircraft technical field, and main purpose is so that the assembly and disassembly of inclining rotary mechanism and fuselage are more convenient, to improve disassembly efficiency.The main technical schemes of the utility model are as follows: the unmanned plane includes inclining rotary mechanism, and the inclining rotary mechanism includes ontology and the first plug division and the first positioning region for being set to the ontology；Fuselage is provided with the second plug division and the second positioning region on the fuselage；Wherein, first plug division and second plug division it is pluggable plug together connection, first positioning region and second positioning region are removably cooperatively connected to prevent to generate relative motion between first plug division and second plug division.The utility model is mainly used for realizing the fast assembling-disassembling between reclining device and fuselage.
Description
Technical field
The utility model relates to aviation aircraft technical fields, in particular to a kind of unmanned plane and inclining rotary mechanism.
Background technique
Tilting rotor wing unmanned aerial vehicle is a kind of aircraft for having both VTOL and fixed-wing model of flight, and reclining device is it
One of core component, reclining device are connect with fuselage, for realizing such unmanned plane in fixed-wing mode and VTOL
Conversion between mode.
It is attached currently, the reclining device of such unmanned plane generallys use the fasteners such as screw with fuselage, when user needs
When dismantling reclining device, must fasteners such as knockout screw first, could will be disassembled with reclining device slave, equally
Ground must just be able to achieve the group of reclining device and fuselage by fasteners such as group cartridge screws when user needs to assemble reclining device
Dress, inconvenient, disassembly efficiency is lower.
Utility model content
In view of this, it is so that verting that the utility model embodiment, which provides a kind of unmanned plane and inclining rotary mechanism, main purpose,
The assembly and disassembly of device and fuselage are more convenient, to improve disassembly efficiency.
In order to achieve the above objectives, the utility model mainly provides the following technical solutions:
On the one hand, the utility model embodiment provides a kind of unmanned plane, comprising:
Inclining rotary mechanism, the inclining rotary mechanism include ontology and the first plug division being arranged on the body and the first positioning
Portion；
Fuselage is provided with the second plug division and the second positioning region on the fuselage；
Wherein, first plug division and second plug division it is pluggable plug together connection, first positioning region and
Second positioning region is removably cooperatively connected to prevent to generate phase between first plug division and second plug division
To movement.
Further, the ontology includes driver, and be electrically connected with the driver is additionally provided on the ontology
One electrical connection-peg；
The electrical connection-peg of can be electrically connected with external electrical appliance module second, second electricity are additionally provided on the fuselage
Property connection-peg electrically plug together and connect with the described first electrical pluggable ground of connection-peg；
The plugging direction of described first electrical connection-peg and the second electrical connection-peg, with first plug division and institute
The plugging direction for stating the second plug division is identical；And first plug division and second plug division be when mutually plugging together or separate,
Described first electrical connection-peg and the second electrical connection-peg are mutually plugged together or are separated.
Further, first plug division includes being set to the ontology and parallel with the surface of the ontology
One inserting column；
Second plug division includes being set to the fuselage and extending along the direction parallel with first inserting column
The first spliced eye；
First inserting column, which plugs together, to be connected in first spliced eye.
Further, first plug division further includes being set to the ontology, and parallel with first inserting column
And the second inserting column identical with the first inserting column extending direction；
Second plug division further includes being set to the fuselage and prolonging along the direction parallel with second inserting column
The second spliced eye stretched；
Second inserting column and plugging together is connected in second spliced eye.
Further, first positioning region includes the positioning deck for being set to the ontology, and the positioning deck includes
Deck ontology and positioning pin with the deck ontology elastic connection；
Second positioning region includes the third spliced eye for being set to the fuselage；
When the positioning pin is mobile relative to the deck ontology, the positioning pin is detached from the third spliced eye；It is described fixed
When position pin resets, the positioning pin is inserted in the third spliced eye.
Further, it is provided with accommodation groove on the deck ontology, elastic component, the deck is provided in the accommodation groove
The end of ontology is provided with the through-hole being connected to the accommodation groove；
The side of the positioning pin is provided with boss, and one end of the positioning pin is inserted in the through-hole, the positioning pin
It is abutted against by the boss and the elastic component；
When the positioning pin is mobile relative to the deck ontology, the positioning pin compresses the elasticity by the boss
Part, in through-hole described in one end retraction of the positioning pin, the positioning pin is detached from the third spliced eye；The positioning pin is in institute
When stating reset under the elastic force effect of elastic component, one end of the positioning pin is revealed in the through-hole, and one end of the positioning pin is inserted
Set on the third spliced eye.
Further, the end of described positioning pin one end is provided with inclined surface；
The chamfered shape of the third spliced eye is adapted with the end profile shape of described positioning pin one end.
On the other hand, the utility model embodiment also provides a kind of inclining rotary mechanism, is used for unmanned plane, including ontology above-mentioned
With the first plug division and the first positioning region being arranged on the body.
By above-mentioned technical proposal, the utility model is at least had the advantages that
Technical solution provided by the embodiment of the utility model, by the way that the first grafting is arranged on the inclining rotary mechanism of reclining device
Portion and the first positioning region, are arranged the second plug division and the second positioning region on fuselage, and realizing to need to assemble reclining device
When on fuselage, the first plug division and the second plug division only need to plug together to connection, and by the first positioning region and the second positioning region
It is cooperatively connected to prevent to generate relative motion between the first plug division and second plug division, reclining device can be realized
With the assembly and connection of fuselage；When needing being disassembled with reclining device slave, the first positioning region and second need to only be determined
Bit position is from and separating the first plug division and the second plug division, reclining device can be realized and separate with the disassembly of fuselage, grasp
Make simple and convenient, improves disassembly efficiency.
Detailed description of the invention
Fig. 1 is a kind of structural schematic diagram of unmanned plane provided by the embodiment of the utility model；
Fig. 2 is the structural schematic diagram of inclining rotary mechanism in Fig. 1；
Fig. 3 is the explosive view that deck is positioned in Fig. 2；
Fig. 4 is the structural schematic diagram that deck is positioned in Fig. 2.
Specific embodiment
To keep the purpose of this utility model, technical solution and advantage clearer, below in conjunction with the excellent of the utility model
The attached drawing in embodiment is selected, the technical scheme in the embodiment of the utility model is further described in more detail.In the accompanying drawings, certainly
Begin to indicate same or similar element or element with the same or similar functions to same or similar label eventually.It is described
Embodiment is the utility model a part of the embodiment, instead of all the embodiments.Below with reference to the implementation of attached drawing description
Example is exemplary, it is intended to for explaining the utility model, and should not be understood as limiting the present invention.It is practical based on this
Embodiment in novel, every other reality obtained by those of ordinary skill in the art without making creative efforts
Example is applied, is fallen within the protection scope of the utility model.The embodiments of the present invention are described in detail with reference to the accompanying drawing.
In the description of the present embodiment, it is to be understood that term " center ", " longitudinal direction ", " transverse direction ", "front", "rear",
The orientation or positional relationship of the instructions such as "left", "right", "vertical", "horizontal", "top", "bottom" "inner", "outside" is based on attached drawing institute
The orientation or positional relationship shown is merely for convenience of description the present embodiment and simplifies description, rather than indication or suggestion meaning
Device or element must have a particular orientation, be constructed and operated in a specific orientation, therefore should not be understood as to the present embodiment
The limitation of protection scope.
As shown in Figure 1, the utility model embodiment provides a kind of unmanned plane, including inclining rotary mechanism, the inclining rotary mechanism packet
Ontology 1 is included, the first plug division 2 and the first positioning region are provided on ontology 1；Fuselage 4 is provided with the second grafting on the fuselage 4
Portion 5 and the second positioning region；Wherein, the first plug division 2 and the second plug division 5 it is pluggable plug together connection, the first positioning region and
Two positioning regions are removably cooperatively connected to prevent to generate relative motion between the first plug division 2 and the second plug division 5.
In some instances, the device that the inclining rotary mechanism of the unmanned plane can vert for control unmanned plane propeller,
So that unmanned plane can have both VTOL model of flight and fixed-wing model of flight, it is provided with 2 He of the first plug division
First positioning region, specifically, the first plug division 2 and the first positioning region can be set the housing outer surface in inclining rotary mechanism, and machine
Body 4 is specifically as follows the wing position of unmanned plane, is provided with the second plug division 5 and the second positioning region, specifically, the second grafting
The housing outer surface at wing position can be set in portion 5 and the second positioning region, when the first plug division 2 and the second plug division 5 plug together
After connection, the first positioning region and the second positioning region are cooperatively connected, so that the first plug division 2 and the second plug division 5 will not generate phase
To movement, inclining rotary mechanism can be firmly installed to the wing position of fuselage 4, realize the assembling of inclining rotary mechanism Yu fuselage 4；When
First positioning region is mutually separated with the second positioning region, after the first plug division 2 is pulled away with 5 phase of the second plug division, inclining rotary mechanism, that is, removable
From in fuselage 4, the disassembly of inclining rotary mechanism Yu fuselage 4 is realized, it is simple to operate.
Unmanned plane provided by the embodiment of the utility model, by the way that the first plug division and the first positioning are arranged on inclining rotary mechanism
The second plug division and the second positioning region is arranged in portion on fuselage, realizes when needing for inclining rotary mechanism to be assembled on fuselage, only
First plug division and the second plug division need to plug together to connection, and by the first positioning region and the second positioning region be cooperatively connected with
It prevents to generate relative motion between first plug division and second plug division, the group of inclining rotary mechanism and fuselage can be realized
Load connects；When needing being disassembled with inclining rotary mechanism slave, only need to by the first positioning region and the second position portion from, with
And separate the first plug division and the second plug division, inclining rotary mechanism can be realized and separated with the disassembly of fuselage, it is simple to operate,
Improve disassembly efficiency.
In some instances, referring to Fig. 1, ontology 1 may include driver, is also provided with and drives on the ontology 1
The electrical connection-peg 7 of the first of device electrical connection；Can be electrically connected with external electrical appliance module second can also be set on the fuselage 4
Electrical connection-peg 8, the second electrical connection-peg 8 are electrically plugged together with the first electrical pluggable ground of connection-peg 7 and are connect；First electrical grafting
First 7 and second electrical connection-peg 8 plugging direction it is identical as the plugging direction of the first plug division 2 and the second plug division 5；And first
When plug division 2 and the second plug division 5 mutually plug together or separate, the first electrical connection-peg 7 and the second electrical connection-peg 8 are successively plugged together
Or separation, wherein the steering engine that driver can vert for the tiliting axis of driving propeller, and external electrical appliance module can be
Flight control system.
It should be noted that said external electrical appliance module can also be the power-supply system that can be mounted on unmanned plane, communication
System or imaging such as spray, propaganda directed to communicate, launching at a variety of load systems, it is not limited here.
It is inserted when assembling inclining rotary mechanism and fuselage 4 by the first plug division 2 and the second plug division 5 according to above-described embodiment
After connecing, the first electrical connection-peg 7 and the second electrical connection-peg 8 be it is pluggable finish, to realize steering engine and fly control and be
The electrical connection of system, moreover, being cooperatively connected by the first positioning region and the second positioning region, it can also be ensured that the first electrical connection-peg
7 will not relatively move with the second electrical connection-peg 8, to guarantee reliable electrical connection between the two；Similarly, work as disassembly
Inclining rotary mechanism and when fuselage 4, by the first positioning region and the second position portion from rear, then by the first plug division 2 and the second grafting
Portion 5 separates, and the first electrical connection-peg 7 can be separated mutually with the second electrical property connection-peg 8, to realize steering engine and flight control system
It disconnects, that is to say, that such structure design, realizing can be complete during inclining rotary mechanism is installed or removed with fuselage 4
At being connected or disconnected between steering engine and flight control system, it is not necessary to steering engine and flight control system are separately connected again, so that inclining rotary mechanism
Steering engine and fuselage 4 flight control system between connect or disconnect same simpler convenience, further improve inclining rotary mechanism
With the disassembly efficiency between fuselage 4.Specifically, the first electrical connection-peg 7 and the second electrical connection-peg 8 all can be aviation insert
Head, and the first electrical connection-peg 7 can be air plug female, the second electrical connection-peg 8 can be air plug male connector.
Wherein, the structure type of the first plug division 2 and the second plug division 5 can there are many, as long as the two may be implemented
Between plug together connection.
In some instances, referring to Fig. 1, the first plug division 2 may include being set to ontology 1 and the surface phase with ontology 1
The first parallel inserting column 21；Second plug division 5 may include being set to fuselage 4 and along the side parallel with the first inserting column 21
To the first spliced eye 51 of extension；First inserting column 21, which plugs together, to be connected in the first spliced eye 51.
In some instances, the first spliced eye 51 can for by being arranged on 4 surface of fuselage, and be provided with perforation its
The first fixture block 41 formation of the slot of both ends of the surface, which is fastened and connected in the surface of fuselage 4, so that slot thereon
The first spliced eye 51 is formed with 4 surface of fuselage, first inserted block 9 can be installed on the surface of ontology 1, it can on first inserted block 9
To be provided with L shape grafting arm, the part parallel with 1 surface of ontology forms the first inserting column 21 on the grafting arm, when assembling is verted
When mechanism, can move inclining rotary mechanism is inserted into the first inserting column 21 thereon in the first spliced eye 51 of fuselage 4, until first
Corresponding site on inserted block 9 is abutted against with the corresponding site on the first fixture block 41, and the first inserting column 21 and the first spliced eye 51 are inserted
It is connected to position, the first plug division 2 can be realized and connect with the second plugging together for plug division 5, structure is simple, and it is easy to operate, and will not be right
Fuselage 4 causes to damage.Wherein, the quantity of the first inserting column 21 can be two or more, and the slot on the first inserted block 9
Quantity can also be two or more.
In some instances, referring to Fig. 1, the first plug division 2 can also include be set to ontology 1, and with the first inserting column
21 second inserting columns 22 parallel and identical with 21 extending direction of the first inserting column；Second plug division 5 can also include setting
In fuselage 4 and along the second spliced eye 52 of the direction extension parallel with the second inserting column 22；Second inserting column 22 and the company of plugging together
It is connected in the second spliced eye 52.
In some instances, second inserting column 22 and the first inserting column 21 can be located at the same surface of ontology 1
Two sides, correspondingly, second spliced eye 52 and the first spliced eye 51 can be located at the two sides of respective surfaces on fuselage 4, with
Further increase the assembling stability of inclining rotary mechanism Yu fuselage 4.Specifically when implementing, surface setting can be set on fuselage 4
There is the second fixture block 42 of the slot for penetrating through its both ends of the surface, which is fastened and connected in the surface of fuselage 4, so that thereon
Slot and 4 surface of fuselage form the second spliced eye 52, the second inserted block can be equipped on the surface of ontology 1, on second inserted block
L shape grafting arm is can be set, the part parallel with 1 surface of ontology forms the second inserting column 22 on the grafting arm, when assembling is inclined
When rotation mechanism, can move inclining rotary mechanism makes the first inserting column 21 thereon and the second inserting column 22 successively be inserted into fuselage 4 respectively
The first spliced eye 51 and the second spliced eye 52 in, until corresponding site and the corresponding portion on the second fixture block 42 on the second inserted block
Position abuts against, and in place, the first plug division 2 and the second plug division 5 can be realized in the second inserting column 22 and 52 grafting of the second spliced eye
Plug together connection, structure is simple, easy to operate, and will not cause to damage to fuselage 4.
In some instances, the first inserting column 21 can be equal with the length of the second inserting column 22, to guarantee the first grafting
Column 21 and 51 grafting of the first spliced eye in place when, the second inserting column 22 and the second spliced eye 52 also can be with grafting in place.
Wherein, the structure type of the first positioning region and the second positioning region can there are many, as long as may be implemented therebetween
It is detachable mating connection.
In some instances, referring to Fig. 1 and Fig. 2, the first positioning region may include the positioning deck 3 for being set to ontology 1, should
Positioning deck 3 may include deck ontology 31 and the positioning pin 32 with 31 elastic connection of deck ontology；Second positioning region can wrap
Include the third spliced eye 6 for being set to fuselage 4；When positioning pin 32 is mobile relative to deck ontology 31, positioning pin 32 is detached from third grafting
Hole 6；When positioning pin 32 resets, positioning pin 32 is inserted in third spliced eye 6.
According to above-described embodiment, when dismantling inclining rotary mechanism, external force can be applied to positioning pin 32 to pull out positioning pin 32
From third spliced eye 6 so that the first positioning region and the second position portion from, then move inclining rotary mechanism so that the first plug division 2 with
Second plug division 5 separation, to realize the disassembly of inclining rotary mechanism；When assembling inclining rotary mechanism, can be applied first to positioning pin 32
Add external force to guarantee that it will not be inserted into third spliced eye 6, then moves inclining rotary mechanism so that the first plug division 2 and the second plug division
5 plug together connection, after 5 grafting in place of the first plug division 2 and the second plug division, remove the external force applied to positioning pin 32 so that fixed
Position pin 32 resets, so that positioning pin 32 is inserted into third spliced eye 6, to realize the assembling of inclining rotary mechanism.Specifically, Ke Yi
Surface is set on fuselage 4 and is provided with the third fixture block 43 for penetrating through the slot of its both ends of the surface, third spliced eye 6 can be set this
On three fixture blocks 43, and positioning deck 3 and can be set in the side of ontology 1, structure is simple, and it is easy to operate, and fuselage 4 will not be made
At damage.
It should be noted that in some instances, referring to Fig. 1, in order to enable the structure of inclining rotary mechanism is simpler compact,
Second inserted block above-mentioned can be the same part with deck ontology 31, that is to say, that the end of deck ontology 31 can be designed in L
Shape is to the at L-shaped grafting arm of shape, and the part parallel with 1 surface of ontology forms the second inserting column 22 above-mentioned on the grafting arm.
In some instances, referring to Fig. 1, in order to guarantee the bonding strength between fuselage 4 and inclining rotary mechanism, above-mentioned second
Electrical connection-peg 8, the first fixture block 41, the second fixture block 42 and third fixture block 43 can be set to 4 enclosure interior of fuselage by pad
Connecting plate 44 connect with 4 shell of fuselage, i.e., connecting plate 44 pad be located at 4 shell inner surface of fuselage, then fastener is successively worn
Cross connecting plate 44 and 4 shell of fuselage respectively with the second electrical connection-peg 8, the first fixture block 41, the second fixture block 42 and third fixture block
43 connections, ensure that the bonding strength between fuselage 4 and inclining rotary mechanism.
In some instances, in order to further convenient for dismounting between fuselage 4 and inclining rotary mechanism, can by the first inserted block 9,
The same surface of ontology 1 is arranged in first electrical connection-peg 7 and positioning deck 3, and the first electrical connection-peg 7 is located at the first inserted block
Between 9 and positioning deck 3, correspondingly, the second electrical connection-peg 8, the first fixture block 41, the second fixture block 42 and third fixture block 43 can
Be arranged in 4 shell of fuselage with the corresponding position on a surface.
In some instances, referring to fig. 2, Fig. 3 and Fig. 4, and combine Fig. 1, accommodation groove can be set on deck ontology 31
311, flexible part 312 can be set in the accommodation groove 311, the end of deck ontology 31 can be set and accommodation groove 311 connects
Logical through-hole 313；The side of positioning pin 32 is provided with boss 321, and one end of positioning pin 32 is inserted in through-hole 313, positioning pin 32
It is abutted against by boss 321 and elastic component 312；When positioning pin 32 is mobile relative to deck ontology 31, positioning pin 32 passes through boss 321
Compress the elastic component 312, in one end retraction through-hole 313 of positioning pin 32, positioning pin 32 is detached from third spliced eye 6；Positioning pin
32 under the elastic force of elastic component 312 acts on when resetting, and one end of positioning pin 32 is revealed in through-hole 313, and one end of positioning pin 32 is inserted
Set on third spliced eye 6.
In some instances, elastic component 312 can be cylindrical spring, and can be connected on the side wall of accommodation groove 311 with screw thread
A screw 314 is connect, so that elastic component 312 is socketed in the outside of screw 314 and can be compressed or be stretched with respect to screw 314, and
The entirety of positioning pin 32 can be Z-shape, and turning point forms boss 321, and one end of the positioning pin 32 is plugged in through-hole 313,
Turning point is connected in the end of spring, meanwhile, for the ease of the control of positioning pin 32, can be arranged in the other end of positioning pin 32
With its one push plate 322 connected vertically, is just realized in this way when user pushes the push plate 322, positioning pin 32 is made to pass through boss
321 compressed springs simultaneously overcome the elastic force of spring to make in one end retraction through-hole 313 of positioning pin 32, so that positioning pin 32
It is detached from third spliced eye 6, and then realizes the component of the first positioning region and the second positioning region；When user decontrols the push plate 322, it is fixed to make
Position pin 32 resets under the resilient force of spring so that one end of positioning pin 32 appears from through-hole 313, so that positioning
Pin 32 is inserted into third spliced eye 6, and then realizes the mating connection of the first positioning region and the second positioning region, and structure is simple, and realization can
It leans on.
In some instances, referring to Fig. 1 and Fig. 3, inclined surface 323 can be set in the end of 32 one end of positioning pin；The
The chamfered shape of three spliced eyes 6 can be adapted with the end profile shape of 32 one end of positioning pin.By being tilted on positioning pin 32
The setting in face 323, while the chamfered shape of third spliced eye 6 being designed as being adapted with the chamfered shape of 32 end of positioning pin,
It realizes in positioning pin 32 and third spliced eye 6 firm without complete grafting, positioning pin 32 can be generated because of unmanned plane operation
Shock effect and third spliced eye 6 is successfully slid by the inclined surface 323 so that positioning pin 32 and third spliced eye 6 are slotting
It is firm to connect, and further ensures the assembling stability between inclining rotary mechanism and fuselage 4.
The utility model embodiment additionally provides a kind of inclining rotary mechanism, including ontology 1, and first is provided on the ontology 1 and is inserted
Socket part 2 and the first positioning region.
It should be noted that inclining rotary mechanism involved in this embodiment can be used described in above-described embodiment unmanned plane
Inclining rotary mechanism structure, concrete implementation and working principle can be found in the corresponding contents in above-described embodiment, and details are not described herein again.
Inclining rotary mechanism provided by the embodiment of the utility model is determined by the way that the first plug division and first is arranged on inclining rotary mechanism
The second plug division and the second positioning region is arranged in position portion on fuselage, realizes when needing for inclining rotary mechanism to be assembled on fuselage,
Only the first plug division and the second plug division need to be plugged together connection, and the first positioning region and the second positioning region are cooperatively connected
To prevent to generate relative motion between first plug division and second plug division, inclining rotary mechanism and fuselage can be realized
Assembly and connection；When needing being disassembled with inclining rotary mechanism slave, only need to by the first positioning region and the second position portion from,
And separate the first plug division and the second plug division, inclining rotary mechanism can be realized and separated with the disassembly of fuselage, side easy to operate
Just, disassembly efficiency is improved.
Finally, it should be noted that above embodiments are only to illustrate the technical solution of the utility model, rather than its limitations；
Although the utility model is described in detail with reference to the foregoing embodiments, those skilled in the art should understand that:
It is still possible to modify the technical solutions described in the foregoing embodiments, or part of technical characteristic is carried out etc.
With replacement；And these are modified or replaceed, various embodiments of the utility model technology that it does not separate the essence of the corresponding technical solution
The spirit and scope of scheme.
Claims (8)
1. a kind of unmanned plane characterized by comprising
Inclining rotary mechanism, the inclining rotary mechanism include ontology and the first plug division and the first positioning region for being set to the ontology；
Fuselage is provided with the second plug division and the second positioning region on the fuselage；
Wherein, first plug division and second plug division it is pluggable plug together connection, first positioning region and described
Second positioning region is removably cooperatively connected to prevent to generate opposite fortune between first plug division and second plug division
It is dynamic.
2. unmanned plane according to claim 1, which is characterized in that
The ontology includes driver, and the electrical connection-peg of first be electrically connected with the driver is additionally provided on the ontology；
The electrical connection-peg of can be electrically connected with external electrical appliance module second is additionally provided on the fuselage, described second electrically inserts
Connector is electrically plugged together with the described first electrical pluggable ground of connection-peg and is connect；
The plugging direction of the first electrical connection-peg and the second electrical connection-peg, with first plug division and described the
The plugging direction of two plug divisions is identical；And first plug division and second plug division are when mutually plugging together or separate, it is described
First electrical connection-peg and the second electrical connection-peg are mutually plugged together or are separated.
3. unmanned plane according to claim 1 or 2, which is characterized in that
First plug division includes being set to the ontology and first inserting column parallel with the surface of the ontology；
Second plug division includes for being set to the fuselage and extending along the direction parallel with first inserting column
One spliced eye；
First inserting column, which plugs together, to be connected in first spliced eye.
4. unmanned plane according to claim 3, which is characterized in that
First plug division further include be set to the ontology, and it is parallel with first inserting column and with described first insert
Connect identical second inserting column of column extending direction；
Second plug division further includes being set to the fuselage and extending along the direction parallel with second inserting column
Second spliced eye；
Second inserting column and plugging together is connected in second spliced eye.
5. unmanned plane according to claim 1 or 2, which is characterized in that
First positioning region includes the positioning deck for being set to the ontology, the positioning deck include deck ontology and with institute
State the positioning pin of deck ontology elastic connection；
Second positioning region includes the third spliced eye for being set to the fuselage；
When the positioning pin is mobile relative to the deck ontology, the positioning pin is detached from the third spliced eye；The positioning pin
When reset, the positioning pin is inserted in the third spliced eye.
6. unmanned plane according to claim 5, which is characterized in that
It is provided with accommodation groove on the deck ontology, elastic component is provided in the accommodation groove, the end of the deck ontology is set
It is equipped with the through-hole being connected to the accommodation groove；
The side of the positioning pin is provided with boss, and one end of the positioning pin is inserted in the through-hole, and the positioning pin passes through
The boss is abutted against with the elastic component；
When the positioning pin is mobile relative to the deck ontology, the positioning pin compresses the elastic component, institute by the boss
It states in through-hole described in one end retraction of positioning pin, the positioning pin is detached from the third spliced eye；The positioning pin is in the bullet
Property part elastic force effect it is lower when resetting, one end of the positioning pin is revealed in the through-hole, and one end of the positioning pin is inserted in
The third spliced eye.
7. unmanned plane according to claim 6, which is characterized in that
The end of described positioning pin one end is provided with inclined surface；
The chamfered shape of the third spliced eye is adapted with the end profile shape of described positioning pin one end.
8. a kind of inclining rotary mechanism, be used for unmanned plane, which is characterized in that including ontology described in any one of claims 1 to 7 and
The first plug division and the first positioning region being arranged on the body.
Priority Applications (2)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201821572617.0U CN209097013U (en) | 2018-09-26 | 2018-09-26 | Unmanned plane and inclining rotary mechanism |
| PCT/CN2019/075082 WO2020062757A1 (en) | 2018-09-26 | 2019-02-14 | Unmanned aerial vehicle and tilting mechanism |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201821572617.0U CN209097013U (en) | 2018-09-26 | 2018-09-26 | Unmanned plane and inclining rotary mechanism |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN209097013U true CN209097013U (en) | 2019-07-12 |
Family
ID=67153555
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201821572617.0U Active CN209097013U (en) | 2018-09-26 | 2018-09-26 | Unmanned plane and inclining rotary mechanism |
Country Status (2)
| Country | Link |
|---|---|
| CN (1) | CN209097013U (en) |
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| US7823827B2 (en) * | 2007-07-11 | 2010-11-02 | Piasecki Frederick W | Vectored thruster augmented aircraft |
| CN106005361B (en) * | 2016-04-07 | 2019-06-28 | 珠海市磐石电子科技有限公司 | Aviation power unit and its flight rack and modular aircraft |
| CN106184734B (en) * | 2016-08-16 | 2018-06-29 | 西安交通大学 | A kind of rotor craft inclining rotary mechanism |
| CN206466160U (en) * | 2016-12-21 | 2017-09-05 | 深圳市道通智能航空技术有限公司 | Detachable horn component and aircraft |
| CN109131871B (en) * | 2018-09-26 | 2019-12-31 | 沈阳无距科技有限公司 | Unmanned aerial vehicle and tilting mechanism |
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